Dynamic Response of Rocket Swirl Injectors, Part II: Nonlinear Dynamic Response-Reference-Cited by-同舟云学术

Dynamic Response of Rocket Swirl Injectors, Part II: Nonlinear Dynamic Response

Published:2011-03 Issue:2 Volume:27 Page:412-421
ISSN:0748-4658
Container-title:Journal of Propulsion and Power
language:en
Short-container-title:Journal of Propulsion and Power

Author:

Ismailov Maksud¹,Heister Stephen D.¹

Affiliation:

1. Purdue University, West Lafayette, Indiana 47907

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Space and Planetary Science,Mechanical Engineering,Fuel Technology,Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.B34045

Reference15 articles.

1. Dynamic Response of Rocket Swirl Injectors, Part I: Wave Reflection and Resonance

2. Park, H. "Flow Characteristics of Viscous High-Speed Jets in Axial/ Swirl Injectors," Ph.D. Thesis,Purdue Univ., West Lafayette, IN, 2005, Chap. 4.

3. Richardson, R. "Linear and Nonlinear Dynamics of Swirl Injectors," Ph.D. Thesis,Purdue Univ., West Lafayette, IN, 2007.

4. Xue, J. "Computational Simulation of Flow Inside Pressure-Swirl Atomizers," Ph.D. Thesis,Univ. of Cincinnati, Cincinnati, OH, 2004.

5. Forced Excitation of Swirl Injectors Using a Hydro-Mechanical Pulsator

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